View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 40910U 15049M 23334.11236046 .00096174 00000-0 14507-2 0 9997
2 40910 97.4481 351.5683 0004107 223.3851 136.7080 15.54425533454494
| Epoch (UTC): | 30 November 2023 02:41:47 |
| Eccentricity: | 0.0004107 |
| inclination: | 97.4481° |
| perigee height: | 401 km |
| apogee height: | 406 km |
| right ascension of ascending node: | 351.5683° |
| argument of perigee: | 223.3851° |
| revolutions per day: | 15.54425533 |
| mean anomaly at epoch: | 136.7080° |
| orbit number at epoch: | 45449 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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